CN109229379B - Takeaway distribution method based on unmanned distribution aircraft - Google Patents
Takeaway distribution method based on unmanned distribution aircraft Download PDFInfo
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- CN109229379B CN109229379B CN201810955849.2A CN201810955849A CN109229379B CN 109229379 B CN109229379 B CN 109229379B CN 201810955849 A CN201810955849 A CN 201810955849A CN 109229379 B CN109229379 B CN 109229379B
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- 238000009826 distribution Methods 0.000 title claims abstract description 107
- 238000000034 method Methods 0.000 title claims abstract description 71
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 18
- 238000003860 storage Methods 0.000 claims description 15
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 14
- 230000009471 action Effects 0.000 claims description 13
- 238000007599 discharging Methods 0.000 claims description 12
- 239000000126 substance Substances 0.000 claims description 9
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- 238000000576 coating method Methods 0.000 claims description 7
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- 238000009825 accumulation Methods 0.000 claims description 3
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- 238000007789 sealing Methods 0.000 claims description 2
- 238000004804 winding Methods 0.000 claims description 2
- 230000000694 effects Effects 0.000 claims 1
- 238000002372 labelling Methods 0.000 abstract 1
- 238000004806 packaging method and process Methods 0.000 abstract 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B64D27/353—
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Abstract
The invention belongs to the technical field of unmanned distribution, and particularly relates to a takeaway distribution method based on an unmanned distribution aircraft, which comprises the following steps: making takeaway according to the order information of the user; packaging and labeling the takeaway; confirming the unmanned delivery aircraft which is idle, and placing the take-out in the unmanned delivery aircraft; delivering the take-out to the customer via the unmanned delivery vehicle; the invention can effectively improve the delivery efficiency of takeaway, is slightly influenced by the environment in the delivery process of the takeaway, can ensure the quality of the takeaway in the delivery process, and can deliver a plurality of takeaway at the same time.
Description
Technical Field
The invention belongs to the technical field of unmanned distribution, and particularly relates to a takeout distribution method based on an unmanned distribution aircraft.
Background
In the current society, with the acceleration of life rhythm, the takeaway industry is gradually prosperous, and especially young people generally like ordering food through network APP; an important link of take-out is delivery, and the goodness of a shop is also related to the delivery speed; the delivery speed is limited by the congestion condition of urban roads, the delivery speed of take-out is greatly reduced when the traffic flow is large, the delivery of take-out is influenced by weather, the delivery speed of take-out is generally low in rainy days, the delivery speed of take-out is improved, and the waiting time of customers is reduced, so that the problem that the take-out industry needs to solve urgently is solved.
Disclosure of Invention
In order to make up for the defects of the prior art, the takeaway distribution method based on the unmanned distribution aircraft provided by the invention adopts the unmanned distribution aircraft to distribute takeaway, so that the influence of urban road congestion on distribution is avoided, the distribution speed is increased, the problem of slow distribution speed in rainy days is solved, the waiting time of customers is shortened, and the goodness of the customers to shops is increased.
The technical scheme adopted by the invention for solving the technical problems is as follows: the invention relates to a takeaway distribution method based on an unmanned distribution aircraft, which comprises the following steps:
the method comprises the following steps: making takeaway according to the order information of the user;
step two: after the takeout is manufactured in the first step, the takeout is packaged and labeled;
step three: after the unmanned aircraft is packaged, determining the idle unmanned aircraft, and placing the take-out in the unmanned aircraft;
step four: after the takeout is placed in the third step, the takeout is sent to the customers through the unmanned distribution aircraft;
the unmanned distribution aircraft in the step two comprises a shell, a floating plate, a connecting rod, a loading plate, a distribution box, a cabin door, a cargo discharging device, a propeller and a motor I; the first cavity and the second cavity are arranged in the shell, the first cavity is positioned above the second cavity, the cross section of the first cavity is triangular, the cross section of the second cavity is rectangular, and water is filled at the bottom of the second cavity, so that when the aircraft turns or is subjected to external acting force, the floating plate and the loading plate are kept horizontal to the ground all the time under the action of the water, the goods are prevented from inclining, and the safety and the stability of the goods during transportation are improved; the floating plate is arranged at the bottom of the second cavity and floats above water; the number of the connecting rods is multiple, the lower ends of the connecting rods are fixed on the floating plate, the springs are arranged at the upper ends of the connecting rods and play a role in damping the loading plate, so that the goods are prevented from being subjected to large vibration in the transportation process, and the safety and the stability of goods transportation are further improved; the loading plate is positioned in the second cavity, the loading plate is arranged above the floating plate through a connecting rod and a spring, a plurality of first rectangular grooves are formed in the loading plate, the loading plate is used for loading cargos, and due to the arrangement of the first rectangular grooves, the aircraft can deliver a plurality of cargos at the same time, so that the delivery efficiency is improved; the distribution box is placed on the loading plate through the first rectangular groove and used for placing goods; the cabin door is hinged to the right side of the shell and used for closing the aircraft; the cargo discharging device is arranged at the top of the second cavity and is used for sending the cargo out of the aircraft; the propeller is fixed above the shell and used for driving the aircraft to fly; the first motor is fixed in the first cavity and used for providing power for the propeller. During operation, goods to be transported are placed in the distribution boxes, and then the distribution boxes are sequentially placed in the first rectangular grooves of the loading plate, so that the first rectangular grooves prevent the distribution boxes from sliding in the transportation process, and the stability and the safety of the goods during transportation are guaranteed; in the transportation process, the cabin door seals the aircraft to prevent goods from falling out of the aircraft, and the propeller drives the aircraft to fly to a destination under the driving of the motor I; the water in the cavity II enables the floating plate and the loading plate to be always kept horizontal to the ground under the action of the water, so that the goods are prevented from inclining when the aircraft turns or is subjected to external acting force in the transportation process, the safety and the stability of the goods in the transportation process are improved, and the goods are prevented from being damaged in the transportation process; the floating plate is connected with the loading plate through the connecting rod and the spring, and meanwhile, the spring plays a role in damping the loading plate and the goods on the loading plate, so that the safety and the stability of the goods in the transportation process are further improved; and finally, after the goods reach the destination, the goods are sent out of the aircraft under the action of the discharging device.
The top of the second cavity is also provided with a T-shaped sliding groove, the existence of the T-shaped sliding groove is convenient for the gear and the second motor to be arranged at the top of the second cavity, the number of the T-shaped sliding grooves is the same as that of the distribution boxes, and the right side of the T-shaped sliding groove is provided with teeth; the cabin door is provided with the same T-shaped sliding chute and teeth relative to the top of the cavity II; the delivery device comprises a gear, a motor II, a winch and a pull rope; the gear is arranged in the T-shaped sliding groove; the second motor is arranged at the top of the second cavity through a gear and is used for driving the gear to move along the teeth on the T-shaped sliding groove; the winch is arranged at the left end of the motor I; one end of the pull rope is wound on the winch, and the other end of the pull rope is connected with the distribution box. During operation, after the goods arrived the destination, the hatch door was opened, T font slide on the hatch door links together with the T font slide on the cavity two, hoist engine rolling stay cord makes the delivery box rise, two rotations of motor make the gear move to the casing along the tooth in the T font spout outward, finally outside moving the delivery box out of the casing, make the delivery box fall to the destination under the action of gravity through emitting the stay cord, thereby the process of automatic shipment has been realized, the screw caused the injury to people when having avoided people to get goods, the time that people got goods has been practiced thrift simultaneously, make the aircraft more intelligent.
A rectangular groove II is formed in the rectangular groove I of the loading plate; the bottom of the distribution box is coated with a magnetic coating; and an electromagnet is arranged in the rectangular groove II and is used for adsorbing or popping up the distribution box. When the distribution box is in work, the magnetic coating and the electromagnet are matched with each other, so that the distribution box is attracted by the electromagnet when goods are transported, the distribution box is more stably fixed on the loading plate, relative motion between the distribution box and the loading plate is avoided, the safety and stability of the goods in the transportation process are improved, the goods cannot be damaged in the transportation process, the quality of the goods is ensured, and the performance of an aircraft is improved; simultaneously, the shipment in-process, when the stay cord of shipment device was pull the delivery box, the electro-magnet changed polarity for the delivery box is more convenient pops out the rectangular groove one of loading board, has improved shipment speed of shipment device.
The upper portion of the shell is conical, and the conical design is used for reducing the resistance of wind and avoiding the accumulation of rainwater. The during operation, conical design makes the aircraft diminish in the resistance that rises in-process and receives, thereby the energy of aircraft has been practiced thrift, and then the effective operating time of aircraft has been improved, and simultaneously, conical design makes the rainwater can't be deposited on the aircraft, avoided the rainwater owing to pile up on the aircraft for a long time, finally have the part to get into in the aircraft, cause the influence to the aircraft, the rainwater has been avoided simultaneously to cause additional load to the aircraft, thereby the energy consumption in the aircraft transportation has been reduced, further long when the transportation of having improved the aircraft, the transport capacity of aircraft has been improved.
The lower part of the shell is hemispherical, and the hemispherical design is used for improving the strength of the shell and reducing the resistance of wind. When the aircraft works, the hemispherical design enables the aircraft to uniformly disperse acting force on each part of the aircraft when the aircraft is subjected to the external acting force, so that the capacity of the aircraft for bearing external pressure is improved, and meanwhile, the hemispherical design enables the internal stress of the aircraft shell to be small, the rigidity to be good and the aircraft shell to be difficult to damage, so that the service life of the aircraft is prolonged; meanwhile, the hemispherical design enables the resistance borne by the aircraft in the transportation process to be smaller, and improves the flight speed of the aircraft, so that the delivery efficiency is improved, and the transportation performance of the aircraft is improved; meanwhile, the reduction of the resistance reduces the energy consumption of the aircraft in the transportation process, effectively improves the working time of the aircraft, and improves the transportation capacity of the aircraft.
A solar cell panel is arranged at the conical part of the upper part of the shell and used for converting solar energy; spherical grooves are uniformly formed in the solar cell panel and are used for reducing the reflection of sunlight by the solar cell panel; and an electric storage module is further arranged in the first cavity and used for storing electric energy generated by the solar cell panel. When the solar energy air vehicle works, the energy of sunlight can be utilized by the air vehicle when the air vehicle is transported in the daytime, so that the energy loss of the air vehicle is effectively saved, the effective transportation time of the air vehicle is prolonged, and the transportation capacity of the air vehicle is improved; meanwhile, the electric energy stored by the electric storage module can also supply power to the aircraft at night, so that the aircraft can work for a long time, and the working efficiency and the performance of the aircraft are effectively improved; the existence of the spherical groove on the solar cell panel reduces the reflection of the solar cell panel to light, effectively improves the utilization rate of the solar cell panel to light energy, and improves the speed of electric energy generated by the solar cell panel, thereby ensuring the supply of energy to the aircraft, further ensuring that the aircraft can work efficiently for a long time, and simultaneously improving the speed of the electric energy stored by the electric storage module; the reduction of light reflection also avoids the aircraft from causing light pollution in the transportation process, and improves the practicability of the aircraft.
And the inner wall of the second cavity is also provided with an activated carbon adsorption module which is used for adsorbing harmful substances in the second cavity. During operation, the active carbon adsorption module adsorbs harmful substances in the second cavity, so that the damage of the harmful substances in the second cavity to the goods is avoided, the quality of the goods is ensured, the cleanness of the inner space of the aircraft is ensured, frequent manual cleaning of the inner part of the aircraft is avoided, and the loss of manpower and material resources is saved.
The invention has the following beneficial effects:
1. according to the takeaway distribution method based on the unmanned distribution aircraft, the unmanned distribution aircraft is adopted to distribute takeaway, so that the influence of urban road congestion on distribution is avoided, the distribution speed is increased, the problem of slow distribution speed in rainy days is solved, the waiting time of customers is shortened, and the goodness of the customers to stores is increased.
2. The takeaway distribution method based on the unmanned distribution aircraft adopts the unmanned distribution aircraft to be matched with the loading plate through the water in the second shell cavity, the floating plate, the connecting rod, the spring and the loading plate, so that the floating plate and the loading plate are always kept horizontal to the ground under the action of the water in the takeaway distribution process, thereby avoiding the takeaway from turning over in the distribution process, ensuring the takeaway quality and quality, and improving the satisfaction degree of customers.
3. According to the takeaway distribution method based on the unmanned distribution aircraft, the unmanned distribution aircraft is matched with the power storage module through the solar cell panel arranged on the aircraft, so that the aircraft has longer effective working time, the distribution capacity and the distribution speed of the aircraft are improved, the distribution time is shortened, and the distribution efficiency is improved.
Drawings
FIG. 1 is a flow chart of the present invention;
FIG. 2 is a front view of the present invention;
FIG. 3 is a cross-sectional view A-A of FIG. 2;
FIG. 4 is a cross-sectional view B-B of FIG. 2;
in the figure: the device comprises a shell 1, a floating plate 2, a connecting rod 3, a loading plate 4, a distribution box 5, a cabin door 6, a cargo discharging device 7, a propeller 8, a first motor 9, a T-shaped chute 11, a solar cell panel 12, an electric power storage module 13, an activated carbon adsorption module 14, an electromagnet 51, a gear 71, a second motor 72, a winch 73 and a pull rope 74.
Detailed Description
A takeaway distribution method based on an unmanned distribution aircraft according to an embodiment of the present invention will be described below with reference to fig. 1 to 4.
As shown in fig. 1 to 3, the takeaway distribution method based on the unmanned distribution aircraft according to the present invention includes the following steps:
the method comprises the following steps: making takeaway according to the order information of the user;
step two: after the takeout is manufactured in the first step, the takeout is packaged and labeled;
step three: after the unmanned aircraft is packaged, determining the idle unmanned aircraft, and placing the take-out in the unmanned aircraft;
step four: after the takeout is placed in the third step, the takeout is sent to the customers through the unmanned distribution aircraft;
the unmanned distribution aircraft in the step two comprises a shell 1, a floating plate 2, a connecting rod 3, a loading plate 4, a distribution box 5, a cabin door 6, a cargo discharging device 7, a propeller 8 and a motor I9; the first cavity and the second cavity are arranged in the shell 1, the first cavity is positioned above the second cavity, the cross section of the first cavity is triangular, the cross section of the second cavity is rectangular, and water is filled at the bottom of the second cavity, so that the floating plate 2 and the loading plate 4 are always kept horizontal relative to the ground under the action of the water when the aircraft turns or is subjected to external acting force, thereby preventing goods from inclining and improving the safety and stability of goods during transportation; the floating plate 2 is arranged at the bottom of the second cavity, and the floating plate 2 floats above water; the number of the connecting rods 3 is multiple, the lower ends of the connecting rods 3 are fixed on the floating plate 2, the springs are arranged at the upper ends of the connecting rods 3, and the springs play a role in damping the loading plate 4, so that the goods are prevented from being subjected to large vibration in the transportation process, and the safety and the stability of goods transportation are further improved; the loading plate 4 is located in the cavity II, the loading plate 4 is mounted above the floating plate 2 through the connecting rod 3 and the spring, the loading plate 4 is provided with a plurality of first rectangular grooves, the loading plate 4 is used for loading cargos, and due to the arrangement of the first rectangular grooves, the aircraft can distribute the cargos at the same time, so that the distribution efficiency is improved; the distribution box 5 is placed on the loading plate 4 through the first rectangular groove, and the distribution box 5 is used for placing goods; the cabin door 6 is hinged on the right side of the shell 1, and the cabin door 6 is used for sealing the aircraft; the cargo discharging device 7 is arranged at the top of the second cavity, and the cargo discharging device 7 is used for discharging cargos out of the aircraft; the propeller 8 is fixed above the shell 1, and the propeller 8 is used for driving the aircraft to fly; the first motor 9 is fixed in the first cavity, and the first motor 9 is used for providing power for the propeller 8. During operation, goods to be transported are placed in the distribution box 5, and then the distribution box 5 is sequentially placed in the first rectangular groove of the loading plate 4, so that the distribution box 5 is prevented from sliding in the transportation process due to the first rectangular groove, and the stability and the safety of the goods during transportation are guaranteed; in the transportation process, the cabin door 6 seals the aircraft to prevent goods from falling out of the aircraft, and the propeller 8 drives the aircraft to fly to a destination under the driving of the motor I9; the water in the cavity II enables the floating plate 2 and the loading plate 4 to be always kept horizontal to the ground under the action of the water, so that the goods are prevented from inclining when the aircraft turns or is subjected to external acting force in the transportation process, the safety and the stability of the goods in the transportation process are improved, and the goods are prevented from being damaged in the transportation process; the floating plate 2 is connected with the loading plate 4 through the connecting rod 3 and the spring, and meanwhile, the spring plays a role in damping the goods on the loading plate 4 and the loading plate 4, so that the safety and the stability of the goods in the transportation process are further improved; and finally, after the goods reach the destination, the goods are sent out of the aircraft under the action of the discharging device.
As shown in fig. 2 and 4, a T-shaped chute 11 is further arranged at the top of the second cavity, the presence of the T-shaped chute 11 facilitates the installation of the gear 71 and the motor second 72 at the top of the second cavity, the number of the T-shaped chutes 11 is the same as that of the distribution boxes 5, and teeth are arranged on the right side of the T-shaped chute 11; the hatch door 6 is provided with the same T-shaped sliding groove 11 and teeth relative to the top of the cavity II; the delivery device 7 comprises a gear 71, a second motor 72, a winch 73 and a pull rope 74; the gear 71 is arranged in the T-shaped sliding groove 11; the second motor 72 is mounted at the top of the second cavity through a gear 71, and the second motor 72 is used for driving the gear 71 to move along the teeth on the T-shaped sliding groove 11; the winch 73 is arranged at the left end of the first motor 9; one end of the pull rope 74 is wound on the winding machine 73, and the other end of the pull rope 74 is connected with the distribution box 5. During operation, after the goods arrived the destination, hatch door 6 was opened, T font slide on the hatch door 6 links together with the T font slide on the cavity two, hoist engine 73 rolling stay cord 74 makes distribution box 5 rise, the rotatory gear 71 that makes of motor two 72 moves outside casing 1 along the tooth in T font spout 11, finally shift out outside distribution box 5 casing 1, make distribution box 5 fall to the destination under the action of gravity through emitting stay cord 74, thereby the process of automatic shipment has been realized, screw 8 causes the injury to people when having avoided people to get goods, the time of people to get goods has been practiced thrift simultaneously, make the aircraft more intelligent.
As shown in fig. 2, a rectangular groove two is arranged on the rectangular groove one of the loading plate 4; the bottom of the distribution box 5 is coated with a magnetic coating; and an electromagnet 51 is arranged in the second rectangular groove, and the electromagnet 51 is used for adsorbing or popping the distribution box 5. When the distribution box is in work, the magnetic coating and the electromagnet 51 are matched with each other, so that the electromagnet 51 attracts the distribution box 5 when goods are transported, the distribution box 5 is more stably fixed on the loading plate 4, the relative motion between the distribution box 5 and the loading plate 4 is avoided, the safety and the stability of the goods in the transportation process are improved, the goods are prevented from being damaged in the transportation process, the quality of the goods is ensured, and the performance of an aircraft is improved; meanwhile, in the delivery process, when the pull rope 74 of the delivery device 7 pulls the delivery box 5, the electromagnet 51 changes the polarity, so that the delivery box 5 is more conveniently popped out of the first rectangular groove of the loading plate 4, and the delivery speed of the delivery device 7 is improved.
As shown in fig. 2, the upper portion of the housing 1 is conical, and the conical shape is designed to reduce wind resistance and prevent accumulation of rainwater. The during operation, conical design makes the aircraft diminish in the resistance that rises in-process and receives, thereby the energy of aircraft has been practiced thrift, and then the effective operating time of aircraft has been improved, and simultaneously, conical design makes the rainwater can't be deposited on the aircraft, avoided the rainwater owing to pile up on the aircraft for a long time, finally have the part to get into in the aircraft, cause the influence to the aircraft, the rainwater has been avoided simultaneously to cause additional load to the aircraft, thereby the energy consumption in the aircraft transportation has been reduced, further long when the transportation of having improved the aircraft, the transport capacity of aircraft has been improved.
As shown in fig. 2, the lower portion of the housing 1 is a hemisphere, and the hemisphere is designed to improve the strength of the housing 1 and reduce the wind resistance. When the aircraft works, the hemispherical design enables the aircraft to uniformly disperse acting force on each part of the aircraft when the aircraft is subjected to the external acting force, so that the capacity of the aircraft for bearing external pressure is improved, and meanwhile, the hemispherical design enables the internal stress of the aircraft shell 1 to be small, the rigidity to be good and the aircraft shell to be difficult to damage, so that the service life of the aircraft is prolonged; meanwhile, the hemispherical design enables the resistance borne by the aircraft in the transportation process to be smaller, and improves the flight speed of the aircraft, so that the delivery efficiency is improved, and the transportation performance of the aircraft is improved; meanwhile, the reduction of the resistance reduces the energy consumption of the aircraft in the transportation process, effectively improves the working time of the aircraft, and improves the transportation capacity of the aircraft.
As shown in fig. 2, a solar cell panel 12 is arranged at a conical part of the upper part of the housing 1, and the solar cell panel 12 is used for converting solar energy; spherical grooves are uniformly formed in the solar cell panel 12 and are used for reducing the reflection of sunlight by the solar cell panel 12; an electric storage module 13 is further arranged in the first cavity, and the electric storage module 13 is used for storing electric energy generated by the solar cell panel 12. When the solar energy air vehicle works, the energy of sunlight can be utilized by the air vehicle when the air vehicle is transported in the daytime by the solar cell panel 12, so that the energy loss of the air vehicle is effectively saved, the effective transportation time of the air vehicle is prolonged, and the transportation capacity of the air vehicle is improved; meanwhile, the electric storage module 13 stores redundant electric energy generated by the solar cell panel 12, so that the waste of electric energy is avoided, and meanwhile, the electric energy stored by the electric storage module 13 can also supply power to the aircraft at night, so that the aircraft can work for a long time, and the working efficiency and the performance of the aircraft are effectively improved; the existence of the spherical groove on the solar cell panel 12 reduces the reflection of the solar cell panel 12 to light, effectively improves the utilization rate of the solar cell panel 12 to light energy, and improves the speed of electric energy generated by the solar cell panel 12, so that the supply of the energy to the aircraft is ensured, the aircraft can work efficiently for a long time, and the speed of storing the electric energy by the electric storage module 13 is improved; the reduction of light reflection also avoids the aircraft from causing light pollution in the transportation process, and improves the practicability of the aircraft.
As shown in fig. 2, an activated carbon adsorption module 14 is further disposed on the inner wall of the second cavity, and the activated carbon adsorption module is used for adsorbing harmful substances in the second cavity. During operation, the harmful substance in the second cavity is adsorbed by the activated carbon adsorption module 14, and the damage of the harmful substance in the second cavity to the goods is avoided, so that the quality of the goods is ensured, the cleanness of the inner space of the aircraft is ensured, frequent manual cleaning of the inner part of the aircraft is avoided, and the loss of manpower and material resources is saved.
The specific operation flow is as follows:
during operation, goods to be transported are placed in the distribution box 5, and then the distribution box 5 is sequentially placed in the first rectangular groove of the loading plate 4, so that the distribution box 5 is prevented from sliding in the transportation process due to the first rectangular groove, and the stability and the safety of the goods during transportation are guaranteed; in the transportation process, the cabin door 6 seals the aircraft to prevent goods from falling out of the aircraft, and the propeller 8 drives the aircraft to fly to a destination under the driving of the motor I9; the water in the cavity II enables the floating plate 2 and the loading plate 4 to be always kept horizontal to the ground under the action of the water, so that the goods are prevented from inclining when the aircraft turns or is subjected to external acting force in the transportation process, the safety and the stability of the goods in the transportation process are improved, and the goods are prevented from being damaged in the transportation process; the connecting rod 3 and the spring enable the floating plate 2 and the loading plate 4 to be connected together, meanwhile, the spring plays a role in damping the goods on the loading plate 4 and the loading plate 4, the safety and the stability of the goods in the transportation process are further improved, and due to the arrangement of the plurality of groups of rectangular grooves in the loading plate 4, the aircraft can deliver a plurality of goods simultaneously, and the delivery efficiency is improved; meanwhile, the distribution box 5 is adsorbed by the electromagnet 51 through the interaction between the electromagnet 51 and the magnetic coating at the bottom of the distribution box 5 during transportation, so that the stability and the safety of goods during transportation are further ensured; finally arrive the destination after, hatch door 6 is opened, T font slide on hatch door 6 links together with the T font slide on the cavity two, hoist engine 73 rolling stay cord 74 pulling delivery box 5, electro-magnet 51 polarity changes makes delivery box 5 pop out rectangle recess one, stay cord 74 pulls up delivery box 5 after the take-up by a certain height, motor two 72 is rotatory to make gear 71 move outside casing 1 along the tooth in T font spout 11, finally shift out delivery box 5 outside casing 1, make delivery box 5 fall to the destination under the action of gravity through releasing stay cord 74, thereby the process of automatic shipment has been realized, screw 8 causes the injury to people when having avoided people to get goods, the time of people to get goods has been practiced thrift simultaneously, make the aircraft more intelligent.
In-process, conical design makes the aircraft diminish in the resistance that rises in-process and receives, thereby the energy of aircraft has been practiced thrift, and then the effective operating time of aircraft has been improved, and simultaneously, conical design makes the rainwater can't be deposited on the aircraft, avoided the rainwater because pile up on the aircraft for a long time, finally have the part to get into in the aircraft, cause the influence to the aircraft, avoided the rainwater to cause additional load to the aircraft simultaneously, thereby the energy consumption in the aircraft transportation has been reduced, further improvement is long in the transportation of aircraft, the transport capacity of aircraft has been improved.
The hemispherical design ensures that the aircraft bears smaller resistance in the transportation process, and improves the flight speed of the aircraft, thereby improving the delivery efficiency and further improving the transportation performance of the aircraft; meanwhile, the reduction of the resistance saves the energy consumption of the aircraft in the transportation process, effectively improves the working time of the aircraft, and improves the transportation capacity of the aircraft.
Due to the existence of the solar cell panel 12, the aircraft can utilize the energy of sunlight during daytime transportation, so that the energy loss of the aircraft is effectively saved, the effective transportation time of the aircraft is prolonged, and the transportation capacity of the aircraft is improved; meanwhile, the electric storage module 13 stores redundant electric energy generated by the solar cell panel 12, so that the waste of electric energy is avoided, and meanwhile, the electric energy stored by the electric storage module 13 can also supply power to the aircraft at night, so that the aircraft can work for a long time, and the working efficiency and the performance of the aircraft are effectively improved; the existence of the spherical groove on the solar cell panel 12 reduces the reflection of the solar cell panel 12 to light, effectively improves the utilization rate of the solar cell panel 12 to light energy, and improves the speed of electric energy generated by the solar cell panel 12, so that the supply of the energy to the aircraft is ensured, the aircraft can work efficiently for a long time, and the speed of storing the electric energy by the electric storage module 13 is improved; the reduction of light reflection also avoids the aircraft from causing light pollution in the transportation process, and improves the practicability of the aircraft.
The active carbon adsorption module 14 adsorbs harmful substances in the second cavity, so that the harmful substances in the second cavity can be prevented from damaging the goods, the quality of the goods is guaranteed, the cleanness of the inner space of the aircraft is guaranteed, frequent manual cleaning of the inner space of the aircraft is avoided, and the loss of manpower and material resources is saved.
While one embodiment of the present invention has been described above, the present invention is not limited to the above embodiment, and various modifications can be made without departing from the scope of the present invention.
(A) In the above embodiment, the floating plate and the loading plate are connected to each other by the link and the spring to connect and absorb the shock of the loading plate, but the present invention is not limited thereto, and the floating plate and the loading plate may be directly connected to each other by the spring to connect and absorb the shock of the loading plate.
Industrial applicability
According to the method, the delivery speed of the takeaway can be effectively improved, and the quality of the takeaway in the delivery process is guaranteed, so that the takeaway delivery method based on the unmanned delivery aircraft is useful in the technical field of unmanned delivery.
Claims (1)
1. A takeaway distribution method based on an unmanned distribution aircraft is characterized in that:
the unmanned distribution aircraft used in the method comprises a shell (1), a floating plate (2), a connecting rod (3), a loading plate (4), a distribution box (5), a cabin door (6), a cargo discharging device (7), a propeller (8) and a motor I (9); a first cavity and a second cavity are arranged in the shell (1), the first cavity is positioned above the second cavity, the section of the first cavity is triangular, the section of the second cavity is rectangular, and water is filled at the bottom of the second cavity; the floating plate (2) is arranged at the bottom of the second cavity, and the floating plate (2) floats above water; the number of the connecting rods (3) is multiple, the lower ends of the connecting rods (3) are fixed on the floating plate (2), and springs are arranged at the upper ends of the connecting rods (3); the loading plate (4) is located in the cavity II, the loading plate (4) is installed above the floating plate (2) through the connecting rod (3) and the spring, a plurality of rectangular grooves I are formed in the loading plate (4), and the loading plate (4) is used for loading goods; the distribution box (5) is placed on the loading plate (4) through the first rectangular groove, and the distribution box (5) is used for placing goods; the cabin door (6) is hinged to the right side of the shell (1), and the cabin door (6) is used for sealing the aircraft; the cargo discharging device (7) is arranged at the top of the second cavity, and the cargo discharging device (7) is used for conveying cargos out of the aircraft; the propeller (8) is fixed above the shell (1), and the propeller (8) is used for driving the aircraft to fly; the first motor (9) is fixed in the first cavity, the first motor (9) is used for providing power for the propeller (8), T-shaped sliding grooves (11) are further formed in the top of the second cavity, the number of the T-shaped sliding grooves (11) is the same as that of the distribution boxes (5), and teeth are arranged on the right side of each T-shaped sliding groove (11); the hatch door (6) is provided with the same T-shaped sliding groove (11) and teeth relative to the top of the cavity II; the delivery device (7) comprises a gear (71), a motor II (72), a winch (73) and a pull rope (74); the gear (71) is arranged in the T-shaped sliding groove (11); the second motor (72) is mounted at the top of the second cavity through a gear (71), and the second motor (72) is used for driving the gear (71) to move along teeth on the T-shaped sliding groove (11); the winch (73) is arranged at the left end of the motor I (9); one end of the pull rope (74) is wound on the winch (73), the other end of the pull rope (74) is connected with the distribution box (5), and a rectangular groove II is formed in the rectangular groove I of the loading plate (4); the bottom of the distribution box (5) is coated with a magnetic coating; an electromagnet (51) is arranged in the rectangular groove II, the electromagnet (51) is used for adsorbing or popping the distribution box (5), the upper part of the shell (1) is conical, the conical design is used for reducing wind resistance and avoiding accumulation of rainwater, the lower part of the shell (1) is hemispherical, and the hemispherical design is used for improving the strength of the shell (1) and reducing wind resistance;
a solar cell panel (12) is arranged at the conical part of the upper part of the shell (1), and the solar cell panel (12) is used for converting solar energy; spherical grooves are uniformly formed in the solar cell panel (12) and are used for reducing the reflection of sunlight by the solar cell panel (12); an electric storage module (13) is further arranged in the cavity I, and the electric storage module (13) is used for storing electric energy generated by the solar panel (12); an activated carbon adsorption module (14) is further arranged on the inner wall of the second cavity and is used for adsorbing harmful substances in the second cavity;
the takeaway distribution method based on the unmanned distribution aircraft comprises the following steps:
the method comprises the following steps: making takeaway according to the order information of the user;
step two: after the takeout is manufactured in the first step, the takeout is packaged and labeled;
step three: after the takeaway is packaged, confirming an idle unmanned distribution aircraft, and placing the takeaway in the unmanned distribution aircraft;
goods to be conveyed are placed in the distribution boxes (5), and then the distribution boxes (5) are sequentially placed in the first rectangular grooves of the loading plate (4), so that the distribution boxes (5) are prevented from sliding in the transportation process due to the first rectangular grooves, and the stability and the safety of the goods during transportation are guaranteed; in the transportation process, the cabin door (6) seals the aircraft to prevent goods from falling out of the aircraft, and the propeller (8) drives the aircraft to fly to a destination under the driving of the motor I (9); the water in the cavity II enables the floating plate (2) and the loading plate (4) to be always kept horizontal to the ground under the action of the water, so that the goods are prevented from inclining when the aircraft turns or is subjected to external acting force in the transportation process, the safety and the stability of the goods in the transportation process are improved, and the goods are prevented from being damaged in the transportation process; the floating plate (2) is connected with the loading plate (4) through the connecting rod (3) and the spring, meanwhile, the spring has a damping effect on the loading plate (4) and goods on the loading plate (4), the safety and stability of the goods in the transportation process are further improved, and due to the arrangement of the plurality of groups of rectangular grooves in the loading plate (4), the aircraft can distribute the goods at the same time, and the distribution efficiency is improved; meanwhile, the distribution box (5) is adsorbed by the electromagnet (51) through the interaction of the electromagnet (51) and the magnetic coating at the bottom of the distribution box (5) during transportation, so that the stability and the safety of goods during transportation are further ensured; after the destination is finally reached, the cabin door (6) is opened, the T-shaped slide way on the cabin door (6) is connected with the T-shaped slide way on the cavity II, the winding machine (73) winds the pull rope (74) to pull the distribution box (5), the polarity of the electromagnet (51) is changed to enable the distribution box (5) to pop out of the rectangular groove I, the pull rope (74) pulls the distribution box (5) to a certain height, the motor II (72) rotates to enable the gear (71) to move towards the outside of the shell (1) along the teeth in the T-shaped slide groove (11), finally the distribution box (5) is moved out of the shell (1), and the distribution box (5) falls to the destination under the action of gravity by releasing the pull rope (74);
step four: and after the takeout is placed in the third step, the takeout is sent to the customers through the unmanned distribution aircraft.
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| CN201810955849.2A CN109229379B (en) | 2018-08-21 | 2018-08-21 | Takeaway distribution method based on unmanned distribution aircraft |
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| CN109229379B true CN109229379B (en) | 2020-12-08 |
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| US10723442B2 (en) * | 2013-12-26 | 2020-07-28 | Flir Detection, Inc. | Adaptive thrust vector unmanned aerial vehicle |
| CN104859812B (en) * | 2015-05-05 | 2017-09-26 | 上海大学 | It is a kind of can automatic adjusument horizontal head |
| CN106708079A (en) * | 2017-02-28 | 2017-05-24 | 南京信息工程大学 | Unmanned aerial vehicle-based takeaway delivery system and method |
| CN206841710U (en) * | 2017-03-18 | 2018-01-05 | 芜湖元一航空科技有限公司 | A kind of unmanned plane with scarer |
| CN106882382A (en) * | 2017-03-24 | 2017-06-23 | 林娟娟 | Unmanned plane loads fast delivery device |
| CN206900661U (en) * | 2017-04-26 | 2018-01-19 | 湖南农飞客农业科技有限公司 | A kind of agricultural unmanned plane |
| CN107175661B (en) * | 2017-05-19 | 2019-11-22 | 北京中兵泰克科技有限公司 | Allocator and system are taken out based on robot and the intelligence of unmanned plane integration of operation |
| CN206734628U (en) * | 2017-05-25 | 2017-12-12 | 成都航空职业技术学院 | A kind of intelligent express delivery dispatching unmanned plane |
| CN107516181A (en) * | 2017-08-30 | 2017-12-26 | 亿航智能设备（广州）有限公司 | Order allocator, device and system |
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